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The FC-1D: The profitable alternative Flying Circus Commercial Aviation GroupThe FC-1D was designed as an advanced solution for a low cost commercial transport meeting or exceeding all of the 1993/1994 AIAA/Lockheed request for proposal requirements. The driving philosophy behind the design of the FC-1D was the reduction of airline direct operating costs. Every effort was made during the design process to have the customer in mind. The Flying Circus Commercial Aviation Group targeted reductions in drag, fuel consumption, manufacturing costs, and maintenance costs. Flying Circus emphasized cost reduction throughout the entire design program. Drag reduction was achieved by implementation of the aft nacelle wing configuration to reduce cruise drag and increase cruise speeds. To reduce induced drag, rather than increasing the wing span of the FC-1D, spiroids were included in the efficient wing design. Profile and friction drag are reduced by using riblets in place of paint around the fuselage and empennage of the FC-1D. Choosing a single aisle configuration enabled the Flying Circus to optimize the fuselage diameter. Thus, reducing fuselage drag while gaining high structural efficiency. To further reduce fuel consumption a weight reduction program was conducted through the use of composite materials. An additional quality of the FC-1D is its design for low cost manufacturing and assembly. As a result of this design attribute, the FC-1D will have fewer parts which reduces weight as well as maintenance and assembly costs. The FC-1D is affordable and effective, the apex of commercial transport design.
Document ID
19950006215
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Meza, Victor J.
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Alvarez, Jaime
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Harrington, Brook
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Lujan, Michael A.
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Mitlyng, David
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Saroughian, Andy
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Silva, Alex
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Teale, Tim
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Date Acquired
September 6, 2013
Publication Date
June 6, 1994
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-197152
NAS 1.26:197152
Report Number: NASA-CR-197152
Report Number: NAS 1.26:197152
Accession Number
95N12628
Funding Number(s)
CONTRACT_GRANT: NASW-4435
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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